Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Alessandro d'Argenio"'
Autor:
Justin George, Kyle Krogh, Steven G. Hagerott, Tom Berger, Justin Howland, James Gresham, Alessandro D'Argenio, Mark B. Tischler, M. Christopher Cotting
Publikováno v:
Journal of Guidance, Control, and Dynamics. 44:1498-1516
Fly-by-wire control laws for a business jet were developed and a handling qualities assessment flight test was conducted on the Calspan Variable Stability System Learjet-25. The control laws, which...
Autor:
M. Christopher Cotting, Kyle Krogh, William R. Gray, Steven G. Hagerott, Tom Berger, Alessandro D'Argenio, Mark B. Tischler, Justin George, Justin Howland, James Gresham
Publikováno v:
AIAA Modeling and Simulation Technologies Conference.
Autor:
M. Christopher Cotting, Tom Berger, Justin Howland, Alessandro D'Argenio, James Gresham, Mark B. Tischler, Justin George, Kyle Krogh, Steven G. Hagerott
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference.
Publikováno v:
Springer Optimization and Its Applications ISBN: 9783319526539
In this chapter we present a survey of location methods based on Nash equilibria for the design of experiments. The solution of the location problem is given in the bi-dimensional case by means of a potential formulation and a Nash game. The most imp
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f3b1d427a434258246b900772b1f9668
https://doi.org/10.1007/978-3-319-52654-6_4
https://doi.org/10.1007/978-3-319-52654-6_4
Publikováno v:
Computational Methods in Applied Sciences ISBN: 9783319115405
In this paper we present a computational methodology to solve the problem of the proper design of the test matrix for an envelope expansion test campaign, where both flutter and systems testing are required (i.e. a new store integration). There are t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f1fd14a9236154297c8d610356e81546
https://doi.org/10.1007/978-3-319-11541-2_26
https://doi.org/10.1007/978-3-319-11541-2_26
Publikováno v:
29th AIAA Applied Aerodynamics Conference.
This paper describes the Design of Experiment to study the laminarturbulent transition phenomenon on a 10° AEDC cone in TransonicSupersonic regime. In particular, the effects of several parameters (as concentrated roughness height, roughness pos